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NASTRAN Based Static CFD-CSM Coupling in FlowSimulator

机译:基于Nastran的静态CFD-CSM耦合在浮动器中

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For high-fidelity fluid-structure interaction simulations different tools are necessary to allow the highest possible accuracy. In this context the data transfer between the aerodynamic surface and the structural model, and the CFD-mesh deformation are the key parameters. This paper shows a methodology to couple different CFD-solvers to the commercial finite element code Nastran. Thereby the coupling scheme can combine different coupling methods, like radial basis function interpolation and structural beam representations, in one coupling matrix. This allows the application of an adequate coupling function for each component of a complex aircraft model. Considering the performance of fluid-structure coupling, the exported spline matrix of a commerical tool is compared to FSAdvancedSplining, a coupling tool integrated into the FlowSimulator software environment. Additionally an update to CFDmesh deformation with radial basis function interpolation and a strategy for control surface deflection is presented.
机译:对于高保真流体结构相互作用模拟模拟不同的工具是允许最高精度的必要工具。在这种情况下,空气动力表面和结构模型之间的数据传输,以及CFD-网格变形是关键参数。本文显示了将不同的CFD求解器耦合到商业有限元码Nastran的方法。由此,耦合方案可以在一个耦合矩阵中组合不同耦合方法,例如径向基函数插值和结构光束表示。这允许在复杂的飞机模型的每个组件中应用足够的耦合功能。考虑到流体结构耦合的性能,将商品工具的导出的样条矩阵与FSAdvancedSplining进行比较,该耦合工具集成在浮动器软件环境中。此外,还提出了具有径向基函数插值的CFDMESH变形的更新和控制表面偏转的策略。

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